View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 61633U 26145.18436220 +.00000000 +00000-0 +28056-4 0 00001
2 61633 43.0010 86.1071 0001137 266.4535 93.6187 15.27579986 08
| Epoch (UTC): | 25 May 2026 04:25:28 |
| Eccentricity: | 0.0001137 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 86.1071° |
| argument of perigee: | 266.4535° |
| revolutions per day: | 15.27579986 |
| mean anomaly at epoch: | 93.6187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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